MBB-ATC500

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Engine Model: MBB-ATC500. Designer: MBB. Propellants: Lox/LH2. Thrust(vac): 441.300 kN (99,208 lbf). Thrust(sl): 392.400 kN (88,215 lbf). Isp: 460 sec. Isp (sea level): 409 sec. Burn time: 318 sec. Chambers: 1. Chamber Pressure: 250.00 bar. Country: Germany. Status: Study 1969. MBB-ATC500 used on Rocket Stages Used on stage: Beta. on launch vehicle: Beta. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.